CN105636657A - Track system for an amusement ride, in particular for a roller coaster or suspension rail - Google Patents
Track system for an amusement ride, in particular for a roller coaster or suspension rail Download PDFInfo
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- CN105636657A CN105636657A CN201480055011.8A CN201480055011A CN105636657A CN 105636657 A CN105636657 A CN 105636657A CN 201480055011 A CN201480055011 A CN 201480055011A CN 105636657 A CN105636657 A CN 105636657A
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- crossbeam
- orbital segment
- rail system
- main beam
- energy
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- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63G—MERRY-GO-ROUNDS; SWINGS; ROCKING-HORSES; CHUTES; SWITCHBACKS; SIMILAR DEVICES FOR PUBLIC AMUSEMENT
- A63G7/00—Up-and-down hill tracks; Switchbacks
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B61—RAILWAYS
- B61B—RAILWAY SYSTEMS; EQUIPMENT THEREFOR NOT OTHERWISE PROVIDED FOR
- B61B3/00—Elevated railway systems with suspended vehicles
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- Engineering & Computer Science (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Rod-Shaped Construction Members (AREA)
- Bridges Or Land Bridges (AREA)
- Train Traffic Observation, Control, And Security (AREA)
- Wind Motors (AREA)
- Transmissions By Endless Flexible Members (AREA)
- Bearings For Parts Moving Linearly (AREA)
- Joining Of Building Structures In Genera (AREA)
- Railway Tracks (AREA)
Abstract
The invention relates to a track system (10) for amusement rides with truss-like track elements (1) which consist of at least one triangular girder system and comprise, as first and second girder element, tracks (2, 3) extending alongside each other and at least one further girder element (4.1), wherein a first stiffening plane (A1) is formed by the tracks (2, 3) and crossbeams (5, 5.1) connecting these tracks (2, 3), and a second and a third stiffening plane (A2, A3) are formed by in each case one track (2, 3) and transverse struts (6, 6.1) connecting same to the at least third girder element (4.1), and, in order to form track sections (1.1,..., 1.7), the crossbeams (5, 5.1) and transverse struts (6) are arranged spaced apart. According to the invention, provision is made that at least one track section (1.1, 1.2, 1.5, 1.6, 1.7) formed by adjacent crossbeams (5, 5.1) with associated transverse struts (6, 6.1) is designed with a stiffening element (7.3) which spans the track section (1.1, 1.2, 1.3, 1.5, 1.6, 1.7) in such a way that a fourth stiffening plane (A4) is formed by the stiffening element (7.3) together with the further girder element (4.1) of the track section (1.1, 1.2, 1.3, 1.5, 1.6, 1.7).
Description
Technical field
The present invention relates to the recreation facility rail system with the truss-like orbit element described in preamble as claimed in claim 1, further relate to the recreation facility with the rail system in the present invention, it is therefore preferable to roller-coaster or hovertrain.
Background technology
This have truss-like orbit element and be found in European patent EP 2156870B1 for the rail system of roller-coaster, and wherein in figure 6, it demonstrates two interconnective orbit elements 1 of rail system 10 in one section of display of rail system.
Summary of the invention
Each orbit element 1 is three girder systems, the track 2 and 3 wherein extended parallel to each other is as the first and second main beam element, and the 3rd main beam element be configured to three-legged structure relative to above-mentioned track and be designed to tension force or pressure elements 4, wherein in the case track 2 and 3 and tension element 4 connect with several parts so that they by crossbeam 5 and 5.1 and lateral struts 6 and 6.1 form orbital segment 1.1-1.7. Crossbeam 5 and 5.1 connects track 2 and 3 and form, with the two track, the face A1 that puts more energy into as distance piece, and track 2 and 3 is connected to be formed second and the 3rd and puts more energy into face A2 and A3 by two lateral struts 6 and 6.1 with tension element 4. The end of crossbeam 5 and 5.1 and track 2 and 3 and end with lateral struts 6 and 6.1 collectively form two summits of triangle, the 3rd summit is formed by the end of the lateral struts 6 and 6.1 being connected to tension element 4.
Crossbeam 5.1 and crossbeam 5 are different in that crossbeam 5.1 and lateral struts associated therewith 6.1 are provided with the column joint 9 of stigma 9.1. Orbit element 1 is connected to be anchored on the setting post of underground by stigma 9.1, so that whole rail system is by these pillar support. These pillars may be designed to be not only erect the mode that direction supports, it is also possible to arranges in any kind of support.
This column joint 9 is designed to have the two dimensional element of triangular-shaped profile, so that this two dimensional element can be connected to crossbeam 5.1 and lateral struts associated therewith 6.1 on silhouette edge.
In order to increase stability and the rigidity of rail system 10, each orbital segment 1.1-1.7 is provided with three diagonal strut 7.1,7.1 and 7.2, it is positioned at first, second, and third and puts more energy into face A1, A2 and A3, and face of putting more energy into described in respectively between diagonal angle bridge joint orbital segment 1.1-1.7. Therefore, such as when orbital segment 1.1, it is arranged in the second two diagonal strut 7.1 putting more energy into face A2 and A3 with the 3rd and will be respectively connecting to track 2 and be connected to two ends of the crossbeam 5.1 of 3 end being connected with tension element 4 of adjacent lateral struts 6 with 7.2, and be arranged in the first diagonal strut 7.0 putting more energy into face A1 and the one end being connected to the crossbeam 5.1 of track 3 is connected to the opposite end, diagonal angle of crossbeam 5, this opposite end, diagonal angle and track 2 form summit.
Each orbit element 1 is not only by flange 4.11 and 4.12 and is connected with each other by the pad of track 2 and 3, and wherein flange 4.11 and 4.12 is threaded connection the end being arranged on tension element 4.
It is an object of the invention to develop further in some way the rail system in type described in background section, make it possible to reach that there is the high fatigue strengths increasing duty cycle number, or more specifically, use identical or modified rail section can realize from tension element larger distance.
This engineering objective is by showing that the rail system of feature disclosed in Patent right requirement 1 is implemented.
This is used for the rail system with the recreation facility of truss-like orbit element and is made up of at least one three girder system, and include parallel extending the track as the first and second main beam element and additional main beam element, wherein first put more energy into the crossbeam formation that face is connected with by these tracks by track; And second and the 3rd put more energy into face respectively through a track and this track is connected at least the 3rd main beam element lateral struts formed; And, in order to form orbital segment, crossbeam and lateral struts are separated setting, according to present invention be characterized in that at least one orbital segment formed by the adjacent crossbeam with lateral struts associated therewith is configured with stiffening elements, its traverse track section is so that the additional main beam element of stiffening elements and orbital segment collectively forms the 4th puts more energy into face.
Put more energy into face owing to this stiffening elements forms the such 4th, so that it may realize higher fatigue strength, so that higher duty cycle number also can be realized.
Put more energy into face to form the 4th, this stiffening elements can traverse track section so that this 4th put more energy into face in orbital segment without along second and the 3rd put more energy into face direction extend, but also can be connected to as required formed orbital segment the crossbeam with lateral struts associated therewith and and be connected to additional main beam element.
Further development according to the present invention, it is especially advantageous for arranging stiffening elements in this way with diagonal angle traverse track section.
Further development according to the present invention, it is provided that stiffening elements, its one end is connected to a crossbeam of orbital segment, and its other end is connected to bonding pad, and the lateral struts joint being associated with another crossbeam is connected to additional main beam element by this bonding pad.
According to a preferred embodiment of the invention, form the 4th stiffening elements in face one end relative with crossbeam of putting more energy into and be connected to the additional main beam element in three girder systems systems, maybe when using four girder systems to unite, be connected in another two girder system. Alternatively, according to further development, it is possible to one end of stiffening elements to be connected in the horizontal line pillar being associated with other crossbeams.
It addition, according to an advantageous embodiment, it is provided that at least one crossbeam is connected to include the column joint of stigma with the lateral struts associated, and formation the 4th stiffening elements putting more energy into face is connected to column joint.
In particular it is preferred that form the 4th stiffening elements putting more energy into face to be connected to the centre of crossbeam.
An advantageous embodiment according to the present invention, at least one orbital segment has the first and second princess posts, its one end is connected to the centre of orbital segment crossbeam, and the other end of traverse track section is respectively connecting to the crossbeam side on the relative crossbeam of orbital segment or the lateral struts associated with this crossbeam. This setting has reached the purpose of strengthened rail element. In this embodiment of the invention, at least one orbital segment preferably has the 3rd princess post, and it connects the centre of two crossbeams of orbital segment.
Additionally, in a further beneficial embodiment, first and/or second and/or the 3rd at least one orbital segment put more energy in face be provided with diagonal strut, the equal traverse track section of diagonal strut.
Still further advantageous embodiment according to the present invention, orbit element is made up of four girder systems, and include the track extended parallel to each other being used as the first and second main beam element, and two additional main beam element, wherein the described in the case the 4th face of putting more energy into is formed by stiffening elements, its one end is connected to crossbeam and other end traverse track section, puts more energy into face so that in the additional main beam element of stiffening elements and orbital segment collectively forms the 4th. Also the 5th the putting more energy into face of mirror image in face of putting more energy into as the described 4th can be formed.
The development further of the present invention provides simple structural design, and wherein stiffening elements is designed to diagonal strut.
In addition, according to another embodiment of the present invention, column joint is designed to have triangular form profile or have the two dimensional element of rectangular profile when the four girder system of use when the three girder system of use, wherein two dimensional element is connected to crossbeam and two lateral struts on profile side in the case, is substantially free of interruption from the teeth outwards.
Meanwhile, the further development according to the present invention, column joint is configured to two dimensional element, and it has triangular-shaped profile and is connected to crossbeam and two lateral struts on profile side, is substantially free of interruption from the teeth outwards. Preferably stigma is arranged at least one main beam element and in the support that is designed to be connected to be preferably used for the rail system of roller-coaster or hovertrain.
The invention rail system with truss-like orbit element can be used for recreation facility, especially roller-coaster or hovertrain, and also can reequip the rail system for vehicle circle in runing.
All trianglees specifically described herein and rectangular configuration relate to the static summit of theory. Theoretical/static summit due to the clearance needed for vehicle chassis or due to produce relevant free space and by movement/change its course (such as, the track 2 and 3 as girder offsets from summit A2 and A3 to A1). Alternatively, all of pillar may also be two dimensional element.
Accompanying drawing explanation
Hereinafter with reference to accompanying drawing, by example embodiment, the present invention is described in detail. Accompanying drawing is shown as:
Fig. 1 is the diagram of the orbit element in the three girder systems according to the present invention;
Fig. 2 is the axonometric chart of the orbit element of three girder systems in the present invention one specific embodiment;
Fig. 3 is the three-dimensional detail view in the A portion in the orbit plane figure of Fig. 2 middle orbit element;
Fig. 4 is the three-dimensional detail view in the A portion in Fig. 2 side view;
Fig. 5 is the axonometric chart of a part for two interconnective orbit elements according to the present invention one example embodiment;
Fig. 6 is the axonometric chart of a part for two interconnective orbit elements according to another example embodiment of the present invention;
Fig. 7 is the schematic perspective view of the orbit element as four girder systems according to the present invention;
Fig. 8 is the axonometric chart of two interconnective orbit elements according to prior art.
Detailed description of the invention
Truss-like orbit element 1 shown in Fig. 1 and 2 is a part for rail system 10, and rail system 10 is by this interconnective multiple orbit elements 1, and can be used for recreation facility, such as roller-coaster or hovertrain.
Fig. 1 is three girder systems compared to Fig. 2 orbit element 1 illustrated in schematic form, it includes the first and second main beam element as track 2 and 3 and another one i.e. the 3rd main beam element 4.1, the 3rd main beam element, it has the function of generated load, is used as tension force or pressure elements. Three main beam element 2,3 and 4.1 are designed to arch and parallel extension. In straight part, main beam element also extends parallel to each other. Two tracks 2 and 3 collectively form first and put more energy into face A1 with crossbeam 5 (it is connected track 2 and 3). Two tracks 2 and 3 are connected to additional main beam element 4.1 by lateral struts 6. In the case, a crossbeam 5 and two lateral struts 6 are arranged in and the plane of track 2 and 3 crosscut at a prescribed interval, and orbit element 1 is divided into orbital segment 1.1,1.2,1.3,1.4 etc. in this way. Meanwhile, track 3 is connected to multiple lateral struts 6 of additional main beam element 4.1 and forms second and put more energy into face A2, and multiple lateral struts 6 that track 2 is connected to additional main beam element 4.1 form the 3rd and put more energy into face A3.
According to the present invention, the 4th face A4 that puts more energy into is formed by stiffening elements 7.3, and stiffening elements is designed to diagonal strut and its diagonal angle traverse track section (see Fig. 1, orbital segment 1.1) in either case. For this, one end of this diagonal strut 7.3 is connected to be formed the crossbeam 5 of orbital segment 1.1, and the other end of this diagonal strut is connected to the join domain of lateral struts 6 and additional main beam element 4.1, therefore it is directly connected to one that is worth in this additional main beam element 4.1 or two lateral struts 6. According to Fig. 1, this diagonal strut 7.3 is connected to the centre of crossbeam 5, but the position that also can diagonal strut 7.3 is connected on crossbeam 5 beyond centre. Use the 4th to put more energy into face A4, not only can improve dynamic load ability, it is possible to improve static state. Additional main beam element 4.1 carries the tension force as kinematic function or pressure as bottom girder.
This stiffening elements 7.3 may be designed to any kind of element, and can by forming two crossbeams 5 of orbital segment 1.1-1.4 and lateral struts associated therewith 6 and the additional main beam element 4.1 in the bonding pad of these lateral struts 6 is connected on main beam element 4.1 any kind of available point of attachment.
In its basic structure, the orbit element 1 in Fig. 2 is equivalent to orbit element known in prior art European patent EP 2156870B1 and the orbit element 1 shown in Fig. 8. But, in the case, realize the 4th according to Fig. 1 also by diagonal strut 7.3 and put more energy into face A4.
In a similar fashion, the orbit element 1 in Fig. 2 includes one or three girder systems, has the first and second main beam element 2 and 3 being respectively designed to track 2 and 3, also there is the 3rd main beam element, or more specifically, be called additional main beam element 4.1, it is designed to tension force and pressure elements. Two tracks 2 and 3 extended parallel to each other are connected with each other, and are formed on the one hand and put more energy into face A1 across the first of crossbeam 5 and 5.1, and on the other hand, are being each attached to additional main beam element 4.1 by lateral struts 6 and 6.1. Track 3 and lateral struts 6 and other main beam element 4.1 collectively form second and put more energy into face A2; And track 2 and lateral struts 6 and additional main beam element 4.1 collectively form the 3rd and put more energy into face A3. The end of additional main beam element 4.1 is formed with flange 4.11 and 4.12, and they are for connecting into rail system 10 by orbit element 1.
In either case, a crossbeam 5 or 5.1 and two lateral struts 6 or 6.1 are set in one plane, this plane along track 2 and 3 or the transverse direction of additional main beam element 4.1 extend, thus producing in this way to form orbital segment 1.1-1.7.
Crossbeam 5.1 and crossbeam 5 are different in that crossbeam 5.1 and lateral struts associated therewith 6.1 are configured with the column joint 9 with stigma 9.1. This stigma 9.1 allows orbit element 1 to be connected to be anchored into the mullion of underground, so that whole rail system is supported by these mullions. It is used as any kind of support arrangement, for instance for hovertrain.
This column joint 9 is designed to have the two dimensional element of triangular-shaped profile, so that this two dimensional element can be connected to crossbeam 5.1 and the lateral struts 6.1 practiced mutually with it by its profile side.
In addition, all orbital segment 1.1-1.7 are provided with diagonal strut 7.1 and 7.2, one end of each diagonal strut is connected to crossbeam 5 or 5.1 and the other end and corresponding orbital segment diagonal angle is bridged to additional main beam element 4.1, and wherein they collectively form a summit with the end of relative lateral struts 6.
Therefore, from the crossbeam 5.1 of adjacent orbit section 1.1 and 1.2, two diagonal strut 7.1 and 7.2 are arranged on both sides, and diagonal strut relative in each case is connected to the additional main beam element 4.1 of the end of orbital segment 1.1 lateral struts relative with 1.2 6. Also correspondingly structure is can be seen that at crossbeam 5.1 place of orbital segment 1.6 and 1.7. Two diagonal strut 7.1 and 7.2 are also connected to adjacent orbit section 1.3 and 1.4, adjacent orbit section 1.4 and 1.5 and the crossbeam 5 of adjacent orbit section 1.5 and 1.6, and diagonal angle extends across each orbital segment to described summit, this summit has relative lateral struts 6 to be formed with additional main beam element 4.1 in either case.
Additionally, also set up the diagonal strut 7.0 of diagonal angle bridge joint orbital segment 1.1-1.5 and orbital segment 1.7 in the plane of track 2 and 3. This diagonal strut 7.0 by by crossbeam 5 or 5.1 and the summit that formed of track 2 be connected to be formed the opposite end, diagonal angle of the crossbeam 5 or 5.1 on summit with track 3.
A portion detail view with reference to Fig. 2, it is shown as the plane graph of track 2 and 3 in figure 3, and Fig. 4 is shown as side view, wherein the diagonal strut 7.3 of traverse track section 1.1 and 1.2 is separately positioned in two orbital segments 1.1 and 1.2 respectively, the stiffening elements of the face A4 that puts more energy into as the 4th. Its one end of the two diagonal strut 7.3 be preferably centered be connected to crossbeam 5.1 their other end with belong to diagonal strut 7.1 and 7.2 be connected to additional main beam element 4.1 end join,, diagonal strut 7.1 and 7.2 is also connected to additional main beam element 4.1 at this place.
Show in fig. 2 using diagonal strut 7.3 as the 4th structure of stiffening elements putting more energy into face, and also seen in adjacent orbital segment 1.6 and 1.7, this diagonal strut 7.3 of each of which is connected to the center of the crossbeam 5.1 connecting two orbital segments 1.6 and 1.7, and diagonal angle bridges each in these orbital segments 1.6 and 1.7 on the direction of additional main beam element 4.1.
Finally, it is also equipped with such diagonal strut 7.3 according to the orbital segment 1.5 of Fig. 2 and is used as the 4th stiffening elements putting more energy into face. This diagonal strut is also connected to connect the centre of the crossbeam 5 of two orbital segments 1.5 and 1.6, and bridges orbital segment 1.5 to the diagonal angle, direction of additional main beam element 4.1.
According to Fig. 2, orbital segment 1.6 design has the first princess post 8.1 and the second princess post 8.2 so that the two princess post 8.1 and 8.2 extends in the plane formed by track 2 and 3. One end of two princess posts 8.1 and 8.2 is connected to crossbeam 5.1 and extends towards one another V-shaped, so that they are connectable to the centre position of adjacent beams 5.
Fig. 5 shows two orbit elements 1, and it is connected with 4.12 by flange 4.11, and its orbital segment 1.6 and 1.7 or 1.1 and 1.2 is structurally corresponding with the orbital segment 1.1 and 1.2 in Fig. 1.
Therefore, connecting two orbital segments 1.6 and 1.7 and crossbeam 5.1 and lateral struts associated therewith 6.1 and be designed as equipped with column joint 9, it has stigma 9.1. Two diagonal strut 7.1 and 7.2 and pair of horns pillar 7.3 be connected to described crossbeam 5.1 and put more energy into as the 4th the stiffening elements of face A4, and diagonal angle extends across orbital segment 1.6 and 1.7 to the node formed by the end of corresponding relatively transverse pillar 6 and additional main beam element 4.1. The orbital segment 1.1 of another orbit element 1 also builds with 1.2 in the way of similar to crossbeam 5.1, and crossbeam 5.1 connects described orbital segment and has the column joint 9 with stigma 9.1; Therefore, these orbital segments are corresponding with those orbital segments 1.1 and 1.2 of Fig. 2 middle orbit 1.
Fig. 6 displays that two orbit elements 1 and 2, and it is connected by flange 4.11 and 4.12, and this is another example embodiment. The orbital segment 1.1 of Fig. 6 middle orbit element 1 builds in the way of identical with the orbital segment 1.6 of Fig. 2 middle orbit 1, except as the 4th put more energy into face A4 stiffening elements diagonal strut 7.3 except, also there are two extra princess posts 8.1 and 8.2. Additionally, except as the 4th put more energy into face A4 stiffening elements diagonal strut 7.3 except, also have the first princess post 8.1 and the second princess post 8.2 to be arranged on the crossbeam 5.1 forming orbital segment 1.1, this crossbeam 5.1 is positioned on the direction of adjacent tracks section 1.2. The respective end of the two princess post 8.1 and 8.2 of orbital segment 1.2 is connected to two ends of crossbeam 5.1, and the V-shaped centre position towards relative crossbeam 5 extends. Adjacent orbit section 1.3 is except having two diagonal strut 7.1 and 7.2, it may have the diagonal strut 7.3 of stiffening elements of the face A4 that puts more energy into as the 4th, but is provided with a diagonal strut 7.0 but not two princess posts 8.1 and 8.2.
In Fig. 6, latter two orbital segment 1.6 and 1.7 of another orbit element 1 also has the diagonal strut 7.3 of stiffening elements of the face A4 that puts more energy into as the 4th, wherein in the case, diagonal strut 7.3 and two diagonal strut 7.1 are connected to orbit element 1 end with 7.2 crossbeam 5 or the crossbeam 5 being connected with two orbital segments 1.6 and 1.7.
From the crossbeam 5 being connected with two orbital segments 1.6 and 1.7, first and second princess post 8.1 and 8.2 1 aspects are connected to the end of crossbeam 5 on the direction of orbital segment 1.6, and the first and second princess posts 8.1 and 8.2 are connected to the end of crossbeam 5 in each case on the direction of orbital segment 1.6 on the other hand. Meanwhile two princess posts 8.1 with 8.2 towards two orbital segments 1.6 with 1.7 each in the middle junction forming V-shape of relative crossbeam 5.
Orbital segment 1.7 has the 3rd princess post 8.3, and it connects the two crossbeam 5 in the centre position of two crossbeams 5.
Fig. 7 shows the orbit element 1 of rail system, and it is formed by four girder system constructings. This four girders system includes the first and second main beam element and two additional main beam element (i.e. the third and fourth main beam element) 4.1 and 4.2, and the first and second main beam element collectively form parallel track 2 and 3. Two tracks 2 and 3 are separated by crossbeam 5, and collectively form first with these crossbeams and put more energy into face A1. Another two main beam element 4.1 is connected by lateral struts 6.2 with 4.2, and is connected to track 2 and 3 by extra lateral struts 6 and puts more energy into face A0 with formation, and itself and the first face A1 that puts more energy into extend in parallel. Other two main beam element 4.1 and 4.2 each respectively with track 3 and 2 and lateral struts associated therewith 6 form second and the 3rd and put more energy into face A2 and A3. Crossbeam 5 and lateral struts 6 and 6.2 are arranged in the multiple planes separated, and each plane is vertical with track 2 and 3, so that therefore orbit element 1 is divided into orbital segment 1.1-1.6. Orbital segment 1.1-1.6 has diagonal strut 7.0,7.1,7.2 and 7.4, is each arranged on and puts more energy in face A1, A2, A3 and A0.
Putting more energy into face A4 to form the 4th, diagonal strut 7.3 is arranged in orbital segment 1.1 and passes through this orbital segment 1.1 as stiffening elements diagonal angle. For this purpose it is proposed, one end of diagonal strut 7.3 is connected to be formed the centre position of crossbeam 5 of orbital segment 1.1, and the relative other end is connected to lateral struts 6 and 6.2 and the join domain of additional main beam element 4.2. In addition, it is possible to the second end of this diagonal element 7.3 is connected to lateral struts 6 and 6.2 and the join domain of additional main beam element 4.1. Meanwhile this diagonal strut 7.3 may be connected directly to additional main beam element 4.1 or 4.2, or is connected to lateral struts 6 or 6.2. Diagonal strut 7.3 can also be connected on crossbeam 5 off-centered position. Additionally, in another orbital segment 1.2-1.6 also by stiffening elements 7.3 realize the 4th and put more energy into face A4.
Finally, in the orbit element 1 being designed to four girder systems, orbital segment 1.1-1.6 can pass through to be arranged on the first princess post 8.1,8.2 and 8.3 putting more energy in the A1 of face and strengthen, just the same with the orbital segment 1.1 and 1.2 or 1.6 and 1.7 according to Fig. 6 middle orbit element 1. Diagonal strut 7.0,7.1,7.2 and 7.3 described in Fig. 2-6, and princess post 8.1,8.2 is connected to crossbeam 5 and 5.1, lateral struts 6 and 6.1 and additional main beam element 4.1 respectively in the way of identical with disclosed in the European patent EP 2156870B1 described in introductory section with 8.3. Therefore being disclosed in this and be integrally incorporated by reference of this patent specification.
In particular, diagonal strut 7.0,7.1,7.2 and 7.3 can be set such that they are without extending directly to additional main beam element 4.1 from crossbeam 5 or 5.1, but such as extends directly to stigma 9 or to the lateral struts 6 or 6.1 junction point region on additional main beam element 4.1. Additionally, diagonal strut 7.0,7.1 and 7.2 without being connected to the centre position of crossbeam 5 or 5.1, and can also be connectable to the middle position of lateral struts 6 or 6.1.
List of numerals:
The orbit element of 1 rail system 10
2 first main beam element, the track of orbit element 1
3 second main beam element, the track of orbit element 1
4.1 extra 3rd main beam element, the tension force of orbit element 1 and pressure elements
The flange of 4.11 tension elements 4
The flange of 4.12 tension elements 4
Extra 4th main beam element of 4.2 orbit elements 1
5 crossbeams
5.1 with the crossbeam of column joint 9
6 lateral struts
6.1 with the lateral struts of column joint 9
7.0 diagonal strut
7.1 diagonal strut
7.2 diagonal strut
7.3 stiffening elements, diagonal strut
7.4 diagonal strut
8.1 first princess posts
8.2 second princess posts
8.3 the 3rd princess posts
9 column joints
The stigma of 9.1 column joints 9
10 rail systems
Claims (15)
1. for the rail system (10) with truss-like orbit element (1) of recreation facility, it is made up of at least one three girder system, including as the first and second main beam element, the parallel track (2 extended mutually, 3), and at least one additional main beam element (4.1), wherein first put more energy into face (A1) by described track (2, 3) with by described track (2, 3) the multiple crossbeams (5 being connected, 5.1) formed, and second and the 3rd put more energy into face (A2, A3) by described track (2, 3) in this track is connected to described in multiple lateral struts (6 of at least the 3rd main beam element (4.1), 6.1) formed, and in order to form multiple orbital segment (1.1, ..., 1.7), multiple crossbeams (5, 5.1) arrange with multiple lateral struts (6) interval,
It is characterized in that:
By adjacent described crossbeam (5,5.1) and described lateral struts (6 associated there, 6.1) at least one orbital segment (1.1,1.2,1.5 formed, 1.6,1.7) being designed to have stiffening elements (7.3), described stiffening elements (7.3) passes through this orbital segment (1.1,1.2,1.3,1.5,1.6,1.7), make described stiffening elements (7.3) and this orbital segment (1.1,1.2,1.3,1.5,1.6,1.7) described additional main beam element (4.1) collectively forms the 4th and puts more energy into face (A4).
2. rail system (10) as described in claim 1,
It is characterized in that:
Described stiffening elements (7.3) diagonal angle passes through described orbital segment (1.1,1.2,1.3,1.5,1.6,1.7).
3. the rail system (10) as described in claim 1 or 2,
It is characterized in that:
One end of described stiffening elements (7.3) is connected to described orbital segment (1.1,1.2,1.3,1.5,1.6,1.7) a crossbeam (5,5.1), and the other end is connected to join domain, and this join domain will with another crossbeam (5,5.1) the described lateral struts (6,6.1) being associated is connected to described additional main beam element (4.1).
4. the rail system (10) as described in claim 1,2 or 3,
It is characterized in that:
Form the described 4th described stiffening elements (7.3) putting more energy into face (A4) and be connected to described additional main beam element (4.1).
5. the rail system (10) as described in claim 1,2 or 3,
It is characterized in that:
Form the described 4th described stiffening elements (7.3) putting more energy into face (A4) and be connected to described lateral struts (6,6.1).
6. the rail system (10) as described in claim 1 or 2,
It is characterized in that:
At least one crossbeam (5.1) and lateral struts associated therewith (6.1) are connected to the column joint (9) including stigma (9.1); And form the described 4th described stiffening elements (7.3) putting more energy into face (A4) and be connected to described column joint (9).
7. such as the rail system (10) described in aforementioned any claim,
It is characterized in that:
Form the described 4th described stiffening elements (7.3) putting more energy into face (A4) and be preferably coupled to described crossbeam (5,5.1) middle position.
8. such as the rail system (10) described in aforementioned any claim,
It is characterized in that:
At least one orbital segment (1.1,1.2,1.6 described, 1.7) there are the first and second princess posts (8.1,8.2), its one end is connected to described orbital segment (1.1,1.2 between two parties, 1.6,1.7) a crossbeam (5,5.1), and it passes through described orbital segment (1.1,1.2,1.6,1.7) it is respectively connecting to described orbital segment (1.1,1.2 with the other end, 1.6,1.7) side of relative crossbeam (5,5.1), or be connected to and described crossbeam (5,5.1) the described lateral struts (6,6.1) being connected.
9. such as the rail system (10) described in aforementioned any claim,
It is characterized in that:
At least one orbital segment (1.1 described, 1.2,1.6,1.7) having the 3rd princess post (8.3), it is at described orbital segment (1.1,1.2,1.6,1.7) centre position of two crossbeams (5,5.1) connects the two crossbeam (5,5.1).
10. such as the rail system (10) described in aforementioned any claim,
It is characterized in that:
Described first and/or second and/or the 3rd puts more energy into face (A1, A2, A3) at least one orbital segment (1.1 described in, ..., 1.7) be built into have all pass through described orbital segment (1.1 ..., 1.7) diagonal strut (7.0), 7.1,7.2,7.4).
11. such as the rail system (10) described in aforementioned any claim,
It is characterized in that:
Described orbit element (1) is four girder systems, and include as the first and second main beam element and the track (2 being generally parallel to each other extension, 3), and two additional main beam element (4.1, 4.2), wherein said 4th puts more energy into face (A4) by stiffening elements (7.3) formation, described stiffening elements (7.3) traverse track section (1.1, 1.2, 1.3, 1.5, 1.6, 1.7) so that described stiffening elements (7.3) and described orbital segment (1.1, 1.2, 1.3, 1.5, 1.6, 1.7) described additional main beam element (4.1, 4.2) in collectively forms the 4th and puts more energy into face (A4).
12. such as the rail system (10) described in aforementioned any claim,
It is characterized in that:
Described stiffening elements is designed to diagonal strut (7.3).
13. the rail system (10) as described in arbitrary in claim 6-11,
It is characterized in that:
Described column joint (9) is designed to two dimensional element, and it has triangular-shaped profile or rectangular profile, and is connected to described crossbeam (5.1) and said two lateral struts (6.1) at its profile side in the way of power cooperation.
14. rail system (10) as described in claim 12,
It is characterized in that:
Described stigma (9.1) is arranged at least one main beam element (4.1 described, 4.2) on, and in order to be connected to the pillar of described rail system (10), described stigma (9.1) is designed to be preferably used for roller-coaster or hovertrain.
15. a recreation facility, it is therefore preferable to roller-coaster or hovertrain, it has the rail system (10) as described in aforementioned any claim.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102013220067.6A DE102013220067B4 (en) | 2013-10-02 | 2013-10-02 | Track system for a ride, especially for a roller coaster or monorail |
| DE102013220067.6 | 2013-10-02 | ||
| PCT/EP2014/070541 WO2015049162A1 (en) | 2013-10-02 | 2014-09-25 | Track system for an amusement ride, in particular for a roller coaster or suspension rail |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105636657A true CN105636657A (en) | 2016-06-01 |
| CN105636657B CN105636657B (en) | 2017-12-29 |
Family
ID=51619200
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201480055011.8A Active CN105636657B (en) | 2013-10-02 | 2014-09-25 | Recreation facility especially roller-coaster or hovertrain rail system |
Country Status (13)
| Country | Link |
|---|---|
| US (1) | US10058788B2 (en) |
| EP (2) | EP3052210B1 (en) |
| JP (1) | JP6280230B2 (en) |
| CN (1) | CN105636657B (en) |
| AU (1) | AU2014331267B2 (en) |
| CA (1) | CA2925044C (en) |
| DE (4) | DE102013220067B4 (en) |
| DK (2) | DK3574968T3 (en) |
| ES (2) | ES2742332T3 (en) |
| HK (1) | HK1223585A1 (en) |
| HU (2) | HUE044711T2 (en) |
| PL (2) | PL3574968T3 (en) |
| WO (1) | WO2015049162A1 (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN107297078A (en) * | 2017-08-04 | 2017-10-27 | 广州市顺宏游乐设备有限公司 | A kind of rotary sliding car |
| CN107694101A (en) * | 2017-11-03 | 2018-02-16 | 国汇机械制造泰州有限公司 | A kind of Wild Mouse segmented tracks design |
| CN110237538A (en) * | 2019-06-04 | 2019-09-17 | 中建八局第三建设有限公司 | A kind of large size roller-coaster construction method of installation |
| CN113926205A (en) * | 2021-11-04 | 2022-01-14 | 广东蕉岭建筑工程集团有限公司 | Roller coaster track supports fixing device |
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|---|---|---|---|---|
| DE102016123928B4 (en) * | 2016-12-09 | 2019-05-29 | Ingenieurbüro Stengel Gmbh | Backbone rail for a roller coaster and roller coaster arrangement |
| CN107794814B (en) * | 2017-11-21 | 2023-08-25 | 中铁第四勘察设计院集团有限公司 | Suspension type single-rail double-line steel track beam system |
| DE102018108182A1 (en) * | 2018-04-06 | 2019-10-10 | Ingenieurbüro Stengel Gmbh | Rails, track piece, and roller coaster arrangement with the same |
| CN108755290A (en) * | 2018-07-27 | 2018-11-06 | 中国五冶集团有限公司 | Full assembly lattice overhead monorail track structure and assembly technology |
| KR101941409B1 (en) * | 2018-09-07 | 2019-01-23 | 알엔비이엔씨 주식회사 | Truss module without slabdeck for guideway vehicle and construction method |
| US11766619B2 (en) | 2019-02-14 | 2023-09-26 | The Gravity Group, LLC | Track for rolling vehicle and methods of fabricating and assembling the track |
| USD976354S1 (en) * | 2020-03-13 | 2023-01-24 | Ingenieurbuero Stengel Gimbh | Roller coaster track section |
| DE102020118049A1 (en) | 2020-07-08 | 2022-01-13 | Ingenieurbüro Stengel Gmbh | Truss rail, and roller coaster arrangement with the same |
| WO2023083479A1 (en) * | 2021-11-15 | 2023-05-19 | Antonio Zamperla S.P.A. | Track segment and track comprising such track segment for an amusement ride |
| KR102493670B1 (en) * | 2022-06-16 | 2023-01-31 | 이엠티씨 주식회사 | Rail system for track vehicles |
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- 2014-09-25 AU AU2014331267A patent/AU2014331267B2/en active Active
- 2014-09-25 EP EP19181056.3A patent/EP3574968B1/en active Active
- 2014-09-25 HU HUE19181056A patent/HUE059866T2/en unknown
- 2014-09-25 DE DE202014011342.4U patent/DE202014011342U1/en active Active
- 2014-09-25 ES ES14772386T patent/ES2742332T3/en active Active
- 2014-09-25 ES ES19181056T patent/ES2927499T3/en active Active
- 2014-09-25 PL PL19181056.3T patent/PL3574968T3/en unknown
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- 2014-09-25 US US15/023,308 patent/US10058788B2/en active Active
- 2014-09-25 WO PCT/EP2014/070541 patent/WO2015049162A1/en active Application Filing
- 2014-09-25 DE DE202014011579.6U patent/DE202014011579U1/en active Active
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Also Published As
| Publication number | Publication date |
|---|---|
| DE102013220067A1 (en) | 2015-04-02 |
| EP3574968A2 (en) | 2019-12-04 |
| AU2014331267B2 (en) | 2017-07-27 |
| CA2925044C (en) | 2018-12-04 |
| HUE059866T2 (en) | 2023-01-28 |
| US10058788B2 (en) | 2018-08-28 |
| DK3574968T3 (en) | 2022-09-05 |
| ES2927499T3 (en) | 2022-11-07 |
| CA2925044A1 (en) | 2015-04-09 |
| ES2742332T3 (en) | 2020-02-13 |
| PL3052210T3 (en) | 2020-03-31 |
| HK1223585A1 (en) | 2017-08-04 |
| CN105636657B (en) | 2017-12-29 |
| DE202014011342U1 (en) | 2019-07-25 |
| PL3574968T3 (en) | 2022-11-07 |
| EP3052210A1 (en) | 2016-08-10 |
| DE102013220067B4 (en) | 2018-10-11 |
| EP3574968B1 (en) | 2022-06-01 |
| WO2015049162A1 (en) | 2015-04-09 |
| EP3052210B1 (en) | 2019-06-26 |
| DE202014011581U1 (en) | 2022-12-16 |
| US20160250560A1 (en) | 2016-09-01 |
| JP2016537155A (en) | 2016-12-01 |
| AU2014331267A1 (en) | 2016-04-14 |
| JP6280230B2 (en) | 2018-02-14 |
| HUE044711T2 (en) | 2019-11-28 |
| DK3052210T3 (en) | 2019-08-26 |
| EP3574968A3 (en) | 2020-02-12 |
| DE202014011579U1 (en) | 2022-11-10 |
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